Portable self powered line mounted high speed camera system for overhead electric power lines

ABSTRACT

A method of locating a fault on a power line conductor includes measuring a change in magnitude from a load current to a fault current with a first “C” loop coil through an electric power line conductor. At least one camera is selected based on a polarity of the load current and the fault current. An image is captured with the at least one camera assembly in the direction of a fault.

CROSS-REFERENCE TO RELATED APPLICATIONS

The application is a divisional of U.S. application Ser. No. 14/101,463 which was filed Dec. 10, 2013, which claims priority to U.S. Provisional Application No. 61/740,517 which was filed on Dec. 21, 2012.

BACKGROUND

The present disclosure relates to a multiple parameter sensor-transmitter/receiver unit which may be installed on or removed from an energized electric power line, such as an overhead power line. With the advent of Smart-Grid applications for electric power systems, there is an ever increasing need for a device that measures electric, mechanical, and environmental parameters of the power line and captures photo images of faults and lightning strokes on power lines.

In order to address the increasing need for monitoring power lines, devices have been developed that attach directly to the power line. These devices generally require a power source, such as batteries or solar panels. When utilizing batteries, regular maintenance must be performed to replace the batteries, which can become costly. When solar panels are used, the device may only be powered during sunny weather conditions and during daylight hours. Therefore, there is a need for a device which is low maintenance and can be constantly powered independent of weather conditions.

Utility companies invest significant capital into power systems and want to protect that investment from damage that could occur during faults, such as when trees fall onto power lines; or when direct lightning strokes contact power lines and equipment and indirect lightning strokes induce high voltage and high magnitude currents in power lines. When a fault occurs, a significant amount of resources can be required to determine the location and extend of damage caused by the fault. Therefore, there is a need for a device that can locate and assess the cause of the fault without requiring significant resources.

SUMMARY

A method of locating a fault on a power line conductor includes measuring a change in magnitude from a load current to a fault current with a first “C” loop coil through an electric power line conductor. At least one camera is selected based on a polarity of the load current and the fault current. An image is captured with the at least one camera assembly in the direction of a fault.

These and other features of the disclosed examples can be understood from the following description and the accompanying drawings, which can be briefly described as follows.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 illustrates a right side view of an example sensor transmitter receiver unit (“STR unit”).

FIG. 2 illustrates a front view of the STR unit of FIG. 1.

FIG. 3 illustrates a cross-sectional view taken along line A-A of FIG. 2.

FIG. 4 illustrates a cross-sectional view taken along line A-A of FIG. 2 with an example hotstick.

FIG. 5 illustrates another cross-sectional view taken along line A-A of FIG. 2 with the example hotstick.

FIG. 5 a illustrates an enlarged view of a keyhole slot.

FIG. 6 illustrates another cross-sectional view taken along line A-A of FIG. 2 engaging a conductor.

FIG. 7 illustrates an example upper magnetic core subassembly.

FIG. 8 illustrates an expanded view of an example upper magnetic core and an example lower magnetic core surrounding the conductor and an example power supply transformer.

FIG. 9 illustrates a schematic view of the line mounted power supply, electronics and transmitter-receiver of the STR unit.

FIG. 10 illustrates an expanded view of the lower magnetic core, example lead screw assembly, and an example hotstick guide tube.

FIG. 11 illustrates the collapsed view of the lower magnetic core, the lead screw assembly, and the hotstick guide tube.

FIG. 12 illustrates a cross-sectional view taken along line B-B of FIG. 2.

FIG. 13 illustrates a cross-sectional view taken along line C-C of FIG. 1.

FIG. 14 illustrates an exploded view of example support blocks mounting the upper magnetic core subassembly and example upper and lower jaws.

FIG. 15 illustrates an exploded view of an upper magnetic core mount and the upper and lower jaws.

FIG. 16 illustrates a front view of the STR unit installed on the conductor with a first camera assembly and a second camera assembly.

FIGS. 17 a-17 d illustrate a fault current camera trigger.

FIG. 18 illustrates a camera trigger logic and fault image data flow diagram.

FIG. 19 a illustrates fault current greater than rated load current.

FIG. 19 b illustrates a load power factor angle.

FIG. 19 c illustrates a depressed voltage, increased fault current phase angle and increased current.

FIGS. 20 a-20 c illustrate a lightning stroke current camera trigger.

FIG. 21 illustrates lightning stroke voltage determination of positive or negative stroke current.

FIG. 22 illustrates a camera trigger logic and lightning stroke image data flow diagram.

FIG. 23 illustrates a left side view of the camera mounted in a lower housing.

FIG. 24 illustrates a back view of the first camera assembly and the second camera assembly mounted in the lower housing.

FIG. 25 illustrates a table of the camera trigger logic.

DETAILED DESCRIPTION

FIGS. 1 and 2 illustrate an example sensor transmitter receiver unit (“STR unit”) 1 installed on a power line conductor C for measuring and monitoring various parameters of the power line conductor C and its environment. The STR unit 1 is formed from a one piece upper housing 2 and a one piece lower housing 3. The lower housing 3 is accepted into a bead 4 formed on a distal end of the upper housing 2. In this example, the bead 4 which is an integral part of the upper housing 2 is formed by machining a portion of the upper housing 2 to form a groove on the inside of the bead 4. The lower housing 3 is secured to the bead 4 and the upper housing 2 by a collar 5. The collar 5 attaches to a hotstick guide tube 13 (FIG. 3) that is secured to the upper housing 2 and extends through the lower housing 3.

In one example, the upper housing 2 and the lower housing 3 are made of aluminum or other suitable electrically conductive material. The material chosen should accommodate subassembly installation without the use of external surface fasteners which could generate corona discharges due to high voltage being applied to the upper housing 2 and the lower housing 3. The upper housing 2 has the advantage of reducing the number of mating surfaces and eliminating mismatches between multiple cast parts which can generate corona discharges and audible noise due to slightly offset sharp edges of the mating surfaces of the adjacent castings.

Referring to FIGS. 3 and 4, before the STR unit 1 is clamped onto the conductor C, a lower jaw 7 is moved to its fully lowered position spaced from upper jaws 6. This allows the conductor C to pass from position “A” of FIG. 3 through a throat T on the left side of the upper housing 2 and onto the upper jaws 6 in position “B” as shown in FIG. 5.

With the lower jaw 7 of the STR unit 1 in its fully lowered position, a specially designed hotstick 10 is inserted into the bottom of the STR unit 1 and inside the hotstick guide tube 13. In this example, the hotstick 10 is made of an electrically insulated material such as fiberglass. The hotstick 10 includes a hotstick driver assembly 9 (FIG. 4) attached to the hotstick 10 with a pin 36. The hotstick 10 provides the required electrical insulation between the hands of the linemen and the energized conductor C. A flexible stirrup assembly 11 (FIG. 4) contains a flexible braided conductor 12 which bends out of the way to allow the hotstick driver assembly 9 to enter a hole in the collar 5. As mentioned earlier, the collar 5 secures the lower housing 3 to the bead 4 on the upper housing 2. The collar 5 is fastened to the hotstick guide tube 13 using the set screw 5 a which is screwed into the collar 5 and into a hole in the hotstick guide tube 13.

With the hotstick 10 and the hotstick driver assembly 9 fully engaged inside the hotstick guide tube 13, the STR unit 1 can be lifted by the lineman with the hotstick 10 onto the conductor C while maintaining the STR unit 1 securely attached to the hotstick 10.

The upper housing 2 includes two jaw inserts 8, shown in FIGS. 5 and 14, located adjacent the throat T and the upper jaws 6. The two jaw inserts 8 include inclined surfaces 8 a and the upper jaws 6 include inclined surfaces 6 a. The angle of incline of the inclined surfaces 8 a matches the angle of the incline of an inclined surface 2 a on the upper housing 2.

The angle of the inclined surfaces 6 a is steeper than the angle of the inclined surfaces 8 a and the inclined surface 2 a to aid in installing the STR Unit 1 on the conductor C. As the conductor C slides across the inclined surfaces 2 a and 8 a and reaches the steeper incline of the inclined surface 6 a, the STR unit 1 will bounce slightly upward and land in a circular notch 6 b of the upper jaws 6 (See FIG. 4). This allows a conductor temperature sensor to be mounted vertically and in the middle inside the upper jaws 6 and initially extends slightly below the circular notch 6 b for the upper portion of the conductor C. The two different inclined surfaces 6 a and 8 a of the jaw inserts 8 and upper jaws 6 prevent the conductor temperature sensor S, shown in FIGS. 3 and 4, from becoming damaged since the conductor C firmly lands vertically in the circular notch 6 b of the upper jaws 6 and pushes the conductor temperature sensor S up to the inside surface of the circular notch 6 b.

In FIG. 3, the lower jaw 7 is located in a pocket P between two legs of a lower magnetic core 14. The lower jaw 7 is held in place with two spring pins 132 and 133 (FIG. 15) located in the lower jaw 7 that snap into two holes 15 in a lower jaw holder 16 (FIGS. 10 and 11) which is attached to a bottom block 19 using two screws 20 (FIG. 3). The bottom block 19 is located adjacent the base of the upper housing 2.

Two identical electrically conductive lower core covers 17 partially surround the two legs of the lower magnetic core 14. The lower core covers 17 are attached to the bottom block 19 on each side of the lower jaw holder 16 using screws 18 of FIG. 3 on the front right side and one set of the screws 18 on the back left side (not shown). The front and back lower jaw holders 16 are both held in place by the four screws 20, two in the front and two in the back. The two legs of the lower magnetic core 14 are totally encased by the two lower core covers 17 and the front and back lower jaw holders 16. Therefore, the lower magnetic core 14 is not exposed to any moisture, such as from rain, snow, and ice that could enter through the throat T of the upper housing 2 (FIG. 3).

The bottom block 19 contains a conical hole 21 in the center which provides a very low friction bearing surface for the semi-circular top of a lead screw 22 (FIG. 3). The lead screw 22 is held in the conical hole 21 with a retainer plate 23 which has a hole in the middle the size of the lead screw 22 diameter and is fastened to the bottom block 19. The lead screw 22 is threaded into the center of a threaded bushing 25. The threaded bushing 25 has a reduced diameter cylindrical lower portion which fits inside the hotstick guide tube 13 and a larger diameter cylindrical top portion of the threaded bushing 25 is supported on the upper end of the hotstick guide tube 13. Both the threaded bushing 25 and the hotstick guide tube 13 are attached to a hotstick guide support 26 using two large through bolts 27 and nuts which are placed through the holes in a bottom support 28.

Referring to FIG. 2, the upper jaws 6 include two spaced apart jaws and the lower jaw 7 includes a single jaw aligned between the two spaced apart upper jaws 6. When lower jaw 7 is clamped onto the conductor C, the conductor C is bent slightly upward as the lower jaw 7 extends upward between the upper jaws 6 creating a bending moment in the conductor C. The bending moment in the conductor C prevents the STR unit 1 from sliding down the conductor C, especially when the STR unit 1 is mounted at the point of attachment adjacent a utility pole or tower where the slope of the conductor C is at its maximum value. Preventing the upper jaws 6 and the lower jaw 7 from sliding down the conductor C at the point of attachment is necessary when the STR unit is being used to measure sag of the power line conductor.

Referring to FIGS. 5 and 5 a, the bottom support 28 includes an upside down “U” shaped cross member and is fastened at each end to the upper housing with two large threaded screws 29 on each side. The threaded bushing 25 has two small vertical holes 25 a drilled through the threaded bushing 25 on each side of the threaded hole in the middle for the lead screw 22. The vertical holes 25 a are countersunk on the top and provide drainage paths for fluid, such as rain water, that can accumulate underneath the bottom block 19 and on top of the bottom support 28 (FIG. 5 a). The water then drains through the two vertical holes 25 a in the threaded bushing 25 and drops on the inside of the hotstick guide tube 13 and out the bottom of the STR unit 1. Therefore, water will not leak into the lower housing 3.

Referring to FIG. 6, the lead screw 22 has a small diameter hotstick guide 30 which is threaded on the inside and is screwed on the bottom of the lead screw 22. A pin 31 keeps the hotstick guide 30 from turning on the lead screw 22. The hotstick guide 30 prevents the inside of a hotstick lead screw driver 33 from coming into contact with the threads on the lead screw 22 and damaging the internal bore of the lead screw driver 33. It also guides the lead screw driver 33 onto the lead screw 22. When the pin 31 engages the lead screw driver 33 the STR unit 1 is ready for installation on the conductor C.

The hotstick driver assembly 9 includes the lead screw driver 33, a hotstick driver coupling 32, a rivet 34, a hotstick sleeve 35, the pin 36, and the hotstick 10. The hotstick 10 of FIG. 4 rests on the rounded portion of the hotstick driver coupling 32 and the rounded inside bottom of the hotstick guide tube 13. This prevents the lead screw driver 33 from applying pressure to the threaded bushing 25 upon installation of the STR unit 1 on the conductor C. The lead screw driver 33 and the hotstick driver coupling 32 are each fastened to the hotstick sleeve 35 by the rivet 34 and the hotstick sleeve 35 is attached to the hotstick 10 with the pin 36. A long narrow vertical slot in the lead screw driver 33 allows the pin 31 of the lead screw 22 to be engaged with the lead screw driver 33 and is free to slide up or down in the vertical slot 37 as the lead screw is turned to tighten the lower jaw 7 on the conductor C or to loosen the lower jaw 7 from the conductor C to remove the STR unit 1.

When the hotstick driver assembly 9 is engaged with the lead screw 22 as shown in FIG. 4, the STR unit 1 is raised to position “A” relative to the height of the conductor C. The STR unit 1 is then moved toward the conductor C so that the conductor C passes through the throat T of the upper housing 2 and into position “B” as shown in FIG. 5. Once the STR unit 1 is fully supported by the conductor C in position “B”, the hotstick driver assembly 9 is turned clockwise by the installer with the hotstick 10 and allowed to drop down from its position in FIG. 4 to a lower position as in FIG. 5. A horizontal keyhole slot 38 of the lead screw driver 33 is now engaged with the pin 31 of the lead screw 22. With the pin 31 in the horizontal keyhole slot 38, the hotstick driver assembly 9 and the hotstick 10 are secured to the STR unit 1.

In this example, an opening and closing mechanism 39 of FIG. 6 extends the lower jaw 7 upward to secure the STR unit 1 on the conductor C. Additionally, the opening and closing mechanism 39 can also retract the lower jaw 7 to remove the STR unit 1 from the conductor C. The opening and closing mechanism 39 includes the lower magnetic core 14, the lower core covers 17, the lower jaw holders 16, the lower jaw 7, spring pins 132 and 133, the bottom block 19, the retainer plate 23, two fasteners 24, the lead screw 22, the hotstick guide 30, and the pin 31.

FIG. 6 illustrates the keyhole slot 38 on the lead screw driver 33 engaged with the pin 31 on the lead screw 22. As the lead screw 22 is turned clockwise, the opening and closing mechanism 39 moves the lower magnetic core 14 toward an upper magnetic core 40. The upper magnetic core 40 has two large compression springs 41 to bias the upper magnetic core 40 downward. The compression springs 41 provide pressure to hold both the upper magnetic core 40 and the lower magnetic core 14 together to reduce the magnetic reluctance caused by air gaps 54 (FIG. 8) between the upper magnetic core 40 and the lower magnetic core 14.

The hotstick driver assembly 9 can continue to be turned clockwise even after the lower magnetic core 14 begins to mate with the upper magnetic core 40 because the compression springs 41 compress at the top of the upper magnetic core 40. The clockwise motion of the hotstick driver assembly 9 can be achieved either manually or with a battery powered drill or another rotating device, until the lower jaw 7 is tightened onto the conductor C. After the STR unit 1 is mounted on the conductor C, the hotstick 10 is turned slightly to the left, or counterclockwise, and the pin 31 will become disengaged from the horizontal portion of the keyhole slot 38. The hotstick 10 is then free to be removed when the pin 31 aligns with the vertical slot 37.

FIGS. 7 and 8 illustrate the bottom of the compression springs 41 are held in alignment in two cylindrical pockets 42 of two identical horizontal upper core blocks 43 which are each used to clamp the upper magnetic core 40 to two identical magnetic horizontal lower core blocks 44. The top of the compression springs 41 are held in place with two projections 49 extending downward on the inside of the upper housing 2. The compression springs 41 are totally enclosed by the upper housing 2 and are protected from the adverse weather which can cause corrosion. The air gaps 54 between the upper and lower magnetic cores 40 and 14 are totally enclosed by the upper housing 2 which prevents the air gaps 54 from becoming corroded due to moisture from the environment. The horizontal upper core blocks 43 and the horizontal lower core blocks 44 are clamped around the upper magnetic core 40 on each side using two through bolts 45 and two nuts 46 in the front and two through bolts 45 and two nuts 46 located in the back of the upper horizontal core blocks 43 and horizontal lower core blocks 44.

When the two large compression springs 41 push the upper core blocks 43 down, the upper magnetic core 40 is prevented from falling out of a left core shoe 50 and a right core shoe 51, by a step 52 located at the bottom of the right core shoe 51 and a step 53 located at the bottom of the left core shoe 50.

When the lower magnetic core 14 mates with the upper magnetic core 40, the lead screw 22 can be turned further clockwise to move the two upper core blocks 43 away from the steps 52 and 53 and further compress the compression springs 41. The lead screw 22 can continue to be turned clockwise and compress the compression springs 41 until the lower jaw 7 and the upper jaws 6 are tight on the conductor C.

Electrical insulating spools 47 are inserted over each of the through bolts 45 and electrical insulating washers 48 are inserted under the head of each through bolt 45 and under each nut 46. The insulating spools 47 and the insulating washers 48 on each of the through bolts 45 prevent shorted electrically conductive paths around the upper magnetic core 40 which is comprised of the four through bolts 45, four nuts 46, the two electrically conductive upper core blocks 43 and the two lower core blocks 44.

When the upper jaws 6 and the lower jaw 7 are firmly tightened on the conductor C, the compression springs 41 are compressed to their maximum distance, and thus the maximum compressive force is also applied to the lower magnetic core 14 and the upper magnetic core 40. This decreases the size of the air gaps 54 between the lower magnetic core 14 and the upper magnetic core 40 and the magnetic reluctance between the lower magnetic core 14 and the upper magnetic core 40. Depending on the size of the conductor C, varying amounts torque can be applied to the hotstick driver assembly 9 to tighten the opening and closing mechanism 39 on the conductor C.

The physical size and shape of the upper jaws 6 and the lower jaw 7 are designed such that approximately the same compressive force is applied to the upper magnetic core 40 and the lower magnetic core 14. In one example, there are five different sets of upper and lower jaws 6 and 7 that can fit different conductor sizes and types ranging from 0.162 inches in diameter and up to 1.17 inches in diameter. The opening and closing mechanism 39 allows the STR unit 1 to be installed on a wide range of conductor diameters without changing the upper jaws 6 and the lower jaws 7 while maintaining sufficient contact between the upper magnetic core 40 and the lower magnetic core 14 to complete the magnetic circuit of the power supply transformer 55 of the STR unit 1 which derives its power from the current flowing through the conductor C to power a power supply module 60 of FIG. 9. Because the STR unit 1 derives power from the conductor C, batteries or solar cells are not required to power the STR unit 1. The STR unit 1 is powered at all times when current is flowing in the conductor C, even at current levels as low as 6.8 amperes and still process data and transmit data at 1 watt power levels because of the low threshold of the power supply module 60.

Maintaining a minimum magnetic reluctance insures that a power supply transformer 55 (FIGS. 8 and 9) will provide the needed secondary voltage V₂ and secondary current I₂ to operate the power supply transformer 55, sensor electronics module 63, and transmitter/receiver 64. The power supply transformer 55 includes the upper magnetic core 40, the lower magnetic core 14, and a coil winding 56. The upper magnetic core and the lower magnetic core form a window W for accepting the conductor C.

The number of secondary turns N₂ of wire on the coil winding 56 are optimized to produce the required secondary voltage V₂ and secondary current I₂ with a minimum of current I₁ in the conductor C. The coil winding 56 is held in place by two coil bobbins 57 which are supported laterally by the two upper core blocks 43 and the two lower core blocks 44. Secondary leads 58 a and 59 a of coil windings 58 and 59, respectively, are connected to the power supply module 60 which maintains the same level of secondary voltage across leads 61 and 62 for the sensor electronics module 63 and the transmitter/receiver 64 even though the primary current may range from 34 amperes up to 1000 amperes. Lower primary currents of 6.8 amperes are achievable with the low threshold current power supply module 60. The power supply module 60 contains an energy storage device 256 (FIG. 13) which can power the transmitter/receiver 64 when the conductor C current ceases to flow. A transmitting and receiving antenna 81 for the on-board transmitter/receiver 64 is mounted on the upper housing 2 (FIG. 12).

Locating the coil winding 56, 58, and 59 on the upper magnetic core 40 allows the heat from the coil winding 56, 58, and 59 to escape through a vent 65 (FIG. 1) in the upper housing 2. When the conductor sensor S located within the STR unit 1 measures the temperature of the conductor C, it is important that the heat from the coil windings 56, 58, and 59 does not affect the temperature of the conductor C or the conductor temperature sensor S, which is in electrical communication with the sensor electronics module 63. As shown in FIG. 6, a thermally insulating barrier 66 located below the coil windings 56, 58, and 59, allows for a more accurate temperature reading of the conductor temperature by blocking heat from the coil windings 56, 58, and 59.

FIGS. 10-12 and 13 illustrate the lower magnetic core 14 with the lower core covers 17, the lead screw 22, the hotstick guide tube 13, and other related parts in both exploded and collapsed views. The hotstick guide tube 13 is anchored at the top with the through bolts 27 that extend through the bottom support 28 and the hotstick guide support 26. A round cylindrical milled slot 67 is located along opposing sides of the top of the hotstick guide tube 13 to accept the through bolts 27 that support the hotstick guide tube 13.

A central hole 70 extends through a base plate support 68 and a base plate 69 for accepting a bottom portion of the hotstick guide tube 13. The base plate support 68 and the base plate 69 are connected to each other with four identical threaded screws 71. The hotstick guide tube 13 is attached to the base plate support 68 and the base plate 69 with set screws 72 and 73. Left and right side panels 76 of FIG. 12 are attached to the base plate support 68 and the bottom support 28 for the lower core 14 with the use of two identical screws 74 extending through the bottom support 28 and the side panel 76 and at the bottom with two identical screws 75 extending through the side panel 76 and the base plate support 68.

The threaded bushing 25 rests on top of the hotstick guide tube 13 and is prevented from turning relative to the hotstick guide tube 13 using a set screw 77. The left and right side panels 76 not only provide added strength, but also provide the physical space to mount the power supply module 60, the transmitter/receiver 64, the sensor electronics module 63, and support left and right lower core guides 78 and 79.

The left lower core guide 78 and a right lower core guide 79 are “U” shaped and guide the opening and closing mechanism 39 such that the lower magnetic core 14 is aligned with the upper magnetic core 40. Each of the left and right lower core guides 78 and 79 are attached to the left and right side panels 76 with four threaded screws 80. The lower housing 3 is placed over the hotstick guide tube 13 at the bottom and fitted up to the base plate 69 and held in place with the collar 5. This means that once the collar 5 is removed, the lower housing 3 can be removed thus allowing access to the power supply module 60, the sensor electronics module 63, and the transmitter/receiver 64 of FIG. 9 mounted inside and on the left and right side panels 76 for easy maintenance and repair.

FIGS. 7 and 12-15 illustrate an upper magnetic core subassembly 40 a mounted to the upper housing 2. The left and right core shoes 50 and 51 support the upper magnetic core 40 such that the upper magnetic core 40 can move freely up and down inside the left and right shoes 50 and 51. The left and right core shoes 50 and 51 are attached to the upper housing 2 using four support blocks 86 and 87 of FIG. 14, right and left upper core guides 90 and 93, and four vertical through bolts 94, 95, 96, and 97.

The upper magnetic core subassembly 40 a can be inserted through the throat T and fastened to the inside of the upper housing 2. A top portion of the upper housing 2 is “C” shaped which provides a surface on the inside for mounting a current sensing device, such as a “C” loop coil 156 for measuring the power line frequency current (60 Hz or 50 Hz) and a “C” loop coil 157 for measuring lightning stroke current (FIGS. 13 and 16).

The right core shoe 51 has two identical threaded holes 82 and 83 on the front and back for a total of four, and left core shoe 50 has two identical threaded holes 84 and 85 on the front and back for a total of four as shown in FIGS. 7 and 14. As shown in FIG. 14, two identical support blocks 86 on the right side are placed on the front and back of the right core shoe 51 and two identical support blocks 87 are placed on the front and back of the left core shoe 50.

To align the two right side support blocks 86 with the two sets of threaded holes 82 and 83 on the right side of the right core shoe 51, threaded screws 88 and 89 are first inserted into the upper and lower holes in the right side upper core guide 90 and then through the two holes in the right support block 86 and screwed into the accommodating threaded holes 82 and 83 of the right core shoe 51. The two left side support blocks 87 are held in alignment with the left core shoe 50 by first inserting two threaded screws 91 and 92 through the other end of the right side upper core guide 90 and then through the holes in the left side support block 87 and screwed into the threaded holes 84 and 85 of the left core shoe 50. The same process is repeated on the back side by connecting support blocks 86 and 87 to the left upper core guide 93 with the backside of the right core shoe 51 and the back side of the left core shoe 50.

The purpose of the upper core guides 90 and 93 is to insure the two long vertical through bolts 94 and 95 placed through the vertical holes in the two right side support blocks 86 and two long vertical through bolts 96 and 97 placed through the vertical holes in the two left side support blocks 87 line up with the four threaded holes in four threaded inserts 98, 99, 100, and 101, which are embedded in the casting of the upper housing 2. The two right side support blocks 86 are prevented from falling down by inserting the back of a right side upper jaw holder 102 and the back of the left side upper jaw holder 103 over the vertical through bolts 94 and 95 and threading nuts 104 and 105 onto the two vertical through bolts 94 and 95 and tightening them down, respectively. The two left side support blocks 87 are held in place by inserting the vertical through bolts 96 and 97 through the front hole in the right side upper jaw holder 102 and the front hole in the left side upper jaw holder 103 and threading two nuts 106 and 107 on the vertical through bolts 96 and 97 and tightening them down, respectively.

Four threaded through standoffs 108, 109, 110, and 111 are screwed onto the four vertical through bolts 94, 95, 96, and 97, respectively. The thermal barrier 66 is placed over the four bottom holes of the standoffs 108, 109, 110, and 111 and screwed to the standoffs 110 and 111 on the front left side with two flat head screws 112 as shown in FIG. 15.

FIGS. 2 and 15 illustrate casting fillers 113 and 114 located on the back left and back right sides of the STR unit 1 and secured with round head screws 115 which are first inserted through holes in the casting fillers 113 and 114 and then through the two back holes on the right and left side of the thermal barrier 66 and into the standoffs 108 and 109, respectively.

After the upper magnetic core subassembly 40 a is mounted, the left and right lower core guides 78 and 79 including the opening and closing mechanism subassembly 39 and the left and right side panels 76 are inserted through the bottom of the upper housing 2 (See FIG. 12). Four screws 29 are inserted through the two holes on the left and the two holes on the right of the bottom support 28 and screwed into the threaded holes of the upper housing 2. It should be noted that during the insertion process, the right lower core guide 79, shown in FIG. 12, slides around the outside surface of the right core shoe 51 and underneath a tab 116 at the top as a weldment on the right upper side of the right core shoe 51.

As shown in FIG. 12, the tab 116 insures that the right lower core guide 79 fits precisely around the outside of the right core shoe 51 to provide a near perfect alignment of the lower magnetic core 14 with the upper magnetic core 40. The precise alignment between the upper magnetic core 40 and the lower magnetic core 14 reduces magnetic reluctance by decreasing the air gaps 54. This results in a decrease in the threshold current for the operation of the power supply module 60.

Referring to FIGS. 14 and 15, the right side upper jaw holder 102 and the left side upper jaw holder 103 support the two upper jaws 6 and the jaw inserts 8. The long vertical through bolts 96 and 97 which are screwed into the threaded inserts 100 and 101 at the top and on the inside of the upper housing 2 fit through top holes 117 and 118 on the back and front of the right side upper jaw holder 102 on the right side. Also, flush mount screws 119 and 120 are inserted on the back and through corresponding holes in the right side upper jaw holder 102 and are screwed into the upper housing. The flush mount screws 119 and 120 are installed before the upper jaws 6 and inserts 8 are mounted to the right side upper jaw holder 102. The same arrangement for mounting the left side upper jaw holder 103 is followed using screws 121 and 122.

Right and left upper jaw keepers 123 and 124 prevent the upper jaws 6 from dropping down on the inside, because spring pins 126 and 127 are located on the outside and when depressed snap into the holes 128 and 129 of the right side upper jaw holder 102. The same procedure is followed with the left upper jaw keeper 124.

The jaw inserts 8 on the right and left sides of the STR unit 1 and in front of the upper jaws 6 are held in place by inserting threaded bolts 130 and 131 into each insert 8 and through the right and left keepers 123 and 124 and screwing into the upper jaw holders 102 and 103. The spring pins 132 and 133 are included in the lower jaw 7 which when depressed snap into the two holes 15 in the lower jaw holder 16.

The transmitting and receiving antenna 81 for the on-board transmitter/receiver 64 shown in FIG. 9 is mounted on the upper housing 2. The antenna 81 is displayed in FIGS. 1 and 2 and is installed on the top left side in FIG. 1. The solar sensor assembly 134 is located at the top of this housing and on its vertical centerline (FIG. 13). The small hole 140 located directly to the right of the conductor C allows access and adjustment of the electric power line sag sensor 140 (FIG. 1).

In one example, the STR unit 1 includes a first camera assembly 141 for capturing images of the left side only of the STR unit 1 as shown in FIG. 2. In another example, the STR unit 1 includes the first camera assembly 141 for viewing electric power line fault and lightning stroke events in a direction pointing from the left side of the STR unit 1 down along the conductor C and a second camera assembly 349 views electric power line fault and lightning stroke events in a direction pointing from the right side of the STR unit 1 down along the conductor C. (See FIGS. 1 and 16).

With the first and second camera assemblies 141 and 349 employed, the rain sensor assembly 138 installed on the right side of the STR unit 1 is replaced with the second camera assembly 349. It is desirable to capture all the near distance (generally less than one mile) photo images of faults and lightning strokes emanating from both directions, because fault and lightning stroke current and voltage waveforms are already being measured by the STR unit 1 independent of the direction from the STR unit 1 the faults and lightning strokes may have originated.

Referring to FIG. 13, there are two “C” loop coils installed inside the STR unit 1. The “C” loop coil 157 on the right side has a small cross-sectional area for measuring the current waveforms of lightning strokes. The “C” loop coil 156 on the left side has a large cross-sectional area for measuring the current waveforms for 50 Hz or 60 Hz steady state load current and 50 Hz or 60 Hz fault current.

To explain how the first and second camera assemblies 141 and 349 capture pictures of faults and lightning strokes from either direction along the conductor C from the STR unit 1, FIGS. 17 a-17 d, 18, 19, 20 a-20 c, 21, and 22 along with the camera trigger logic of FIG. 25 is used. FIG. 17 a shows the “C” loop coil 156 partially surrounding the conductor C. When the 50 Hz or 60 Hz steady state load current enters from the right side of the conductor C and points in a direction toward the polarity mark 65 located on the outside of the upper housing 2 of FIGS. 2 and 13, the current is emanating from a source and continuing to a load. This direction of current flow has been defined as positive polarity.

As shown in Case I in FIG. 17 b, the load current arrow points to the left or downstream toward the load. When a fault occurs on the line (e.g. a tree falls on the line) to the left of the STR unit 1 at time t=0, the 50 Hz or 60 Hz fault current will (in most cases) have a magnitude higher than the 50 Hz or 60 Hz steady state load current. The sensor electronics module 63 of FIG. 9, which is sampling the 50 Hz or 60 Hz load current waveform at a speed of 360 samples per cycle, will sense this abrupt change in magnitude from the “C” loop coil 156 output and send a trigger signal 350 to the first camera assembly 141 on the left side to capture the picture of the fault as indicated in FIG. 25 and the flow diagram of FIG. 18.

Since the flow of post fault current, or current flow after the fault occurs, is in the same direction as the flow of load current, or pre-fault current, then both of these currents have a positive polarity (+). The Case I represented in FIG. 17 b, where the STR unit 1 measures voltage V and current I at a location downstream of the source, the power flow arrow or load current points downstream toward a fault.

Case II represented in FIG. 17 c illustrates the load current arrow pointing downstream to the left (or positive polarity), but at time t=0, there is a change in the polarity of the fault current waveform of 180 degrees, as indicated by the fault current arrow now pointing to the right in FIG. 17 c. This indicates that the fault has occurred upstream from the STR unit 1 and has a negative polarity (−) as shown in FIG. 25. The sensor electronics module 63 of FIG. 9 senses both a change in polarity of the fault current and an abrupt change in the magnitude of the current waveform. The software of the sensor electronics module 63 performs this function by comparing the slope of the pre-fault current waveform at the instant in time (t=0−) just before the fault occurs at t=0 with the slope of the fault current waveform after the fault occurs, or t=0+.

Referring to Case II current waveform of FIG. 17 c, the load current at t=0 should have gone up with a positive slope, as shown by the dotted portion of the load current waveform, but instead the fault current waveform has a negative slope beginning at t=0. When this change in polarity and this dramatic increase in current magnitude occurs, the sensor electronics module 63 sends a trigger signal 351 to the second camera assembly 349 on the right side to take a picture of the upstream fault as shown in FIGS. 18 and 25.

The sensor electronics module 63 possesses a fault direction feature, because if there is no change in polarity of the current waveform after the fault occurs then the direction of the fault from the STR unit 1 is downstream (i.e., away from the [SOURCE]). If there is a change in polarity of the current waveform after the fault occurs then the fault is upstream from the STR unit 1 (i.e., toward the [SOURCE]). If multiple STR units 1 are installed on the circuit, then the STR units 1 can be used to locate where the fault occurred on the circuit.

Additionally, the STR unit 1 has a transmitter/receiver 64 which not only transmits data to remote locations but also can receive data from these locations as shown in FIG. 9. This additional feature allows trigger levels for various measured parameters to be sent from remote locations 352 to the STR unit 1 transmitter/receiver 64 as shown in FIG. 18.

Remotely adjustable triggers 353 shown in FIG. 18, may be fixed values or rate of change values of a specific measured parameter. In the case of the measured fault current waveforms, the expected magnitude of these waveforms vary depending on where the fault occurs on the circuit. At the source end of the circuit, the fault current magnitude will be higher than the magnitude measured by an STR unit 1 located downstream of the source. The reason for this is because the impedance at the source is lower than the impedance downstream on the circuit. Therefore, different pre-selected fault current level settings are sent from a remote location or locations 352 to different STR units 1 installed on the circuit.

For distribution applications, an example of these pre-selected fault current levels might be 20,000 amperes rms, 10,000 amperes rms, 5,000 amperes rms, and 2,000 amperes rms. The different pre-selected levels insure the fault current waveforms are fully recorded by the sensor electronics module 63 without the waveform being cutoff at the top of the scale if the pre-selected value is too low, or the waveform being too small if the pre-selected value is too high. The pre-selected levels of fault current values are used to produce 0 to 4.011 volts output after the measured currents from the “C” loop coils 156 and 157 are signal conditioned by the sensor electronics module 63.

As shown in FIG. 17 d, the steady state maximum rated load current is 1000 amperes rms and at this value of measured current by the “C” loop coil 156 the signal conditioned output voltage V₀₃ is +4.011 volts peak. The maximum fault current is 20,000 amperes rms, and at this value of measured current by the “C” loop coil 156 the signal conditioned output voltage is 4.011 volts peak. If however, other pre-selected levels of fault current are sent to the STR units from the remote locations 352 then these are also automatically scaled by the sensor electronics module 63 to produce a voltage output V₀₃ of +4.011 volts peak for that pre-selected level.

If the STR unit 1 also measures the steady state line to line or line to neutral voltage, the voltage will become depressed during a fault as shown in the line to neutral voltage measurement in FIG. 19 a. The typical remotely adjustable trigger level for fault voltage is 0.90 per unit of nominal rated voltage. When the voltage drops down to 0.90 per unit or lower, then this indicates a fault is occurring. In addition, since the sensor electronics module 63 is also recording both voltage and current waveforms, it also determines the phase angle between the voltage and current. As shown in FIG. 19 c, the fault current phase angle θ_(f) is much greater than the load power factor angle θ in FIG. 19 b. So, with the voltage measurement added, there are at least four indications a fault is occurring: 1) increased current magnitude; 2) depressed voltage; 3) increased phase angle between the voltage and current phases; and 4) asymmetrical line currents.

Once the first camera assembly 141 or the second camera assembly 349 has taken a picture of the fault, image data 354 or 355 shown in FIG. 18 is sent to the sensor electronics module 63 which in turn sends processed image data 356 to the transmitter/receiver 64. The processed image data including the captured image or images is then sent to the remote locations 352. The first camera assembly 141 and the second camera assembly 349 are supplied with the low voltage (12 volt dc) power from the power supply electronics module 60 through two leads 61 and 62 as shown in FIGS. 9 and 18. The first camera assembly 141 and the second camera assembly 349 are normally powered by batteries for consumer applications. However, here there is no need to change out these batteries when they fail, because the first camera assembly 141 and the second camera assembly 349 are always powered when current is flowing in the power line. The power supply 60 is backed up with the energy storage device 256 as shown in FIG. 13.

For capturing lightning stroke images, the “C” loop coil 157 is used as shown in FIGS. 20 a-20 c. When the lightning stroke current waveform as shown in Case III (FIG. 20 b) is arriving from the right side of the STR unit 1 and is travelling toward the polarity mark 65 (FIG. 20 a), the lightning stroke current will have a positive polarity. Case III shows two lightning stroke current waveforms, one with a positive current waveform, and one with a negative current waveform. It is assumed that a +200 kA stroke which strikes the electric power line splits equally and travels down the line in opposite directions. The recorded positive stroke of +100 kA, after having been measured by the “C” loop coil 157 and signal processed through the sensor electronics module 63, results in a low level dc voltage peak output value of +3.997 volts with its zero reference value at +1.998 volts. The reason for this offset of +1.998 volts is to allow for a peak negative lightning stroke value of −100 kA, and after having been signal processed, results in a peak value of 0.000 volts. The signal processed data outputs allows for the display of either a positive or negative stroke with a positive polarity, that is current travelling into the right side of the STR unit 1.

A positive polarity, positive or negative lightning stroke waveform, requires the trigger 357, shown in FIG. 22, of the second camera assembly 349 on the right side to capture the lightning stroke which occurred to the right of the STR unit 1.

There are two types of lightning strokes which can occur. A direct stroke to the electric power line or an indirect stroke which does not contact the conductor C, but induces a current and voltage in the conductor C due to its close proximity to the conductor C. The first camera assembly 141 and the second camera assembly 349 will capture the images of both direct strokes and indirect strokes in close proximity to the conductor C. The sensor electronics module 63 is sampling the lightning stroke waveform data from the “C” loop coil 157 at a very fast speed of 20 MHz or 20 million samples per second. As shown in FIG. 22, captured image data 358 is sent from the second camera assembly 349 on the right side back to the sensor electronics module 63 which in turn sends this data through a line 359 to the transmitter/receiver 64 and is then transmitted via the antenna 81 to the remote location 352.

In Case IV shown in FIG. 21, a different phenomenon takes place which requires additional information. When the positive or negative lightning stroke current waveform with a peak value of +100 kA or −100 kA travels down the conductor C and approaches the left side of the STR unit 1, the “C” loop coil 157 will measure the current and after having been signal processed by the sensor electronics module 63 will produce an output voltage of +0.000 volts for the peak value of the positive stroke of +100 kA, and will produce an output voltage +3.997 volts for the negative stroke of −100 kA. In other words, the two waveforms have become inverted from what is shown in FIG. 20 because the waveforms have arrived on the opposite side of the polarity mark 65 and therefore, have a negative polarity.

The STR unit 1 also measures and signal processes the positive and negative lightning stroke voltage waveforms via the sensor electronics module 63 as shown in FIG. 21. For this example, the STR unit 1 measures up to a maximum positive peak voltage of +110 kV and a maximum negative peak voltage of −110 kV. These values were selected because the maximum BIL (Basic Impulse Insulation Level) of the surge block 164 is 113 kV.

If a 9 kV rms lightning arrester is applied in the case of the 4800 V system voltage delta connected power system, then a 200,000 ampere maximum peak lightning stroke resulting in 100,000 amperes at the lightning arrester would possess a maximum discharge voltage for the arrester of only 53 kV. Again, as stated earlier, it is assumed the lightning stroke current of 200,000 amperes will split equally into 100,000 amperes and travel in opposite directions along the surface of the conductor C. Since this maximum discharge voltage for this 9 kV arrester rating of 53 kV is well below the 113 kV BIL rating of the surge block 164, then there is a very low probability of insulation failure for the surge block 164.

Referring back to FIG. 21, the selection of a +110 kV lightning stroke or a −110 kV lightning stroke are the maximum values that would be expected that the STR unit 1 voltage measuring system would see even if the lightning arrester failed. When the +100 kA stroke arrived at the “C” loop coil 157 of FIG. 20, it was inverted due to the change in polarity from positive to negative. If the voltage measured after having been processed by the sensor electronics module 63 is positive, then the logic shown in FIG. 25 and in the sensor electronics module 63 knows the +100 kA stroke is in fact positive (not negative) and must have arrived on the left side of the STR unit 1 opposite to the polarity mark 65. Therefore the first camera assembly 141 on the left side is triggered via line 360 to capture photo data of the lightning stroke appearing on the left side of the STR unit 1. The photo data is sent to sensor electronics module 63 using a signal line 361.

The same logic applies to the negative peak lightning stroke current waveforms of −100 kA shown in FIG. 20. When this waveform arrives on the left side of the STR unit 1 and the “C” loop coil 157 measures the current, the signal processing performed by sensor electronics module 63 will have resulted in a +100 kA peak stroke. However, the camera trigger logic of FIG. 25, to which is built into the sensor electronics module 63, recognizes that if the voltage waveform results in a +0.008 peak voltage output as shown in FIG. 21, then the +100 kA lightning stroke peak current waveform must have been a −100 kA peak waveform arriving from the left side of the STR unit 1, because the +0.008 peak voltage output must have been created by a −100 kA peak waveform.

There can only be a positive voltage created by a positive lightning stroke current waveform and a negative voltage created by a negative lightning stroke current waveform. Therefore, for the negative −100 kA lightning stroke arriving on the left side of the STR unit 1, the logic in the sensor electronics module 63 will cause a trigger signal to travel through line 360 (FIG. 22) to initiate the first camera assembly 141 on the left side to capture the −100 kA stroke on the left side of the STR unit 1.

The first camera assembly 141 and the second camera assembly 349 are electrostatically and electromagnetically shielded using a shield 338 as shown in FIGS. 23 and 24. The shield 338 protects the first and second camera assemblies 141 and 349 from producing corona discharges when the STR unit 1 is mounted on high voltage conductors C. The shield 338 includes a clear glass cover 330 with an undercoating of a transparent electrically conducting substrate 297 which is mounted in a bezel 340 of FIGS. 23 and 24. The substrate 297 is grounded to the lower housing 3. Camera lens 362 of the first camera assembly 141 shown in FIG. 23 has a clear view through the glass cover 330 and down the conductor C when mounted on the conductor C. The same is true for second camera assembly 349 of FIG. 24. Each of the first and second camera assemblies is mounted to the lower portion of the side panels of the lower housing 3. The first camera assembly 141 is mounted flush on the left side panel 308 and the second camera assembly 349 on the right side is mounted flush on the right side panel 76 of FIG. 24.

As indicated in FIG. 24, the first camera assembly 141 includes a first telephoto lens 363 and the second camera assembly includes a second telephoto lens 364. The first and second telephoto lens 363 and 364 can be controlled to take close up pictures of far-away lightning strokes and faults.

The first and second camera assemblies 141 and 349 have automatic exposure control based on the intensity of the lightning stroke or fault and possess the characteristics of low lux sensitivity and a very high frames per second speeds to capture lightning strokes which can rise to their peak current values within approximately 0.5 to 1.5 microseconds. Since the STR unit 1 has an accurate time clock as part of an on board global positioning system, then each photo becomes time stamped so that analysis of these events can be related to power line equipment failures or malfunctions.

Since the STR unit 1 is powered by the conductor C current and the associated power supply electronics module 60 including the energy storage device 256 of FIG. 13, then pictures can be taken at night of lightning strokes and fault events without depending on solar panels which may not be operational. Having lightning stroke pictures of equipment and line flashovers and lightning strokes to electric power line equipment are very beneficial in determining how to design lightning protection systems. Since the STR unit 1 measures both the current and voltage waveforms of direct and indirect lightning strokes, and pictures are taken of same then more precise analysis of power line equipment failures and prediction of future failures due to lightning events is more readily available.

Although the first and second assemblies 141 and 349 have thus been described as taking digital photos of events, they can also be live video cameras powered using the same power supply electronics module 60 for viewing in real time potential hazards to the line from trees during high winds, galloping line conductors, ice formation, effects of hurricane winds on the integrity of the lines and their supporting structures, and terrorist activities.

The preceding description is exemplary rather than limiting in nature. Variations and modifications to the disclosed examples may become apparent to those skilled in the art that do not necessarily depart from the essence of this disclosure. The scope of legal protection given to this disclosure can only be determined by studying the following claims. 

What is claimed is:
 1. A method of locating a fault on a power line conductor comprising: mounting a sensor transmitter receiver unit (STR unit) on the power line conductor; measuring a change in magnitude from a load current to a fault current with a first “C” loop coil at least partially surrounding an electric power line conductor; selecting at least one camera on each STR unit based on a polarity of the load current and the fault current; determining the location of the fault by comparing the polarity of the fault current and the load current measured by the STR unit; and capturing an image with the at least one camera assembly in the direction of a fault.
 2. The method of claim 1 wherein the at least one camera assembly includes a first camera assembly and a second camera assembly.
 3. The method of claim 2 including sending a trigger signal to activate the first camera assembly or the second camera assembly based on the polarity of the load current and the fault current.
 4. The method of claim 3 including selecting the at least one camera pointed in the direction of the load current when the polarity of the fault current is positive and in the same direction as the load current.
 5. The method of claim 4 including selecting the at least one camera pointed in an opposite direction of the load current when the polarity of the fault current is negative and opposite to the direction of the load current.
 6. The method of claim 1, including mounting multiple STR units on the power line conductor and determining the location of the fault by comparing the polarity of a fault current and a load current of each of the plurality of STR units.
 7. The method of claim 1 including transmitting the image to a remote location with a transmitter receiver unit and an antenna.
 8. A method of locating a fault on a power line conductor comprising: transmitting a pre-selected fault current level from a remote location with a transmitter receiver unit and an antenna to the transmitter receiver unit mounted on the electric power line conductor via the antenna, wherein the pre-selected levels are used by a sensor electronics module to compare measured load current to an expected magnitude of a fault current with an abrupt change in magnitude to determine the presence of a fault on the electric power line conductor; measuring a change in magnitude from a load current to a fault current with a first “C” loop coil at least partially surrounding an electric power line conductor; selecting at least one camera based on a polarity of the load current and the fault current; and capturing an image with the at least one camera assembly in the direction of a fault.
 9. The method of claim 8 wherein pre-selected levels include expected fault current levels and expected depressed voltages which will occur during faults on the electric power line conductor and are used by the sensor electronics module in addition to the measured and expected fault current to determine the presence of a fault on the electric power line conductor.
 10. The method of claim 9 wherein a fault current phase angle obtained from a fault current waveform and a fault voltage waveform during a fault is used by the sensor electronics module, in addition to the pre-selected levels to detect the presence of the fault on the electric power line conductor.
 11. The method of claim 1, wherein the image is a video image.
 12. The method of claim 1 including measuring a lightning stroke current with a second “C” loop coil and comparing the load current and a lightning stroke current polarity.
 13. The method of claim 12 including comparing a measured positive lightning stroke voltage which can only be created by a measured positive stroke current and a measured negative lightning stroke voltage which can only be created by a measured negative stroke current.
 14. The method of claim 13 including determining a direction of the lightning stroke by which camera is initiated to capture the image.
 15. The method of claim 1 wherein the at least one camera assembly is electrostatically shielded by a transparent material including an electrically conductive substrate mounted within an electrically conducting corona free bezel which is mounted to a housing for preventing corona discharges when the housing is mounted on the electric power line conductor. 